EP3381602B1 - Hybridbauteil mit mehreren kernen und verfahren zur behandlung eines bauteils - Google Patents

Hybridbauteil mit mehreren kernen und verfahren zur behandlung eines bauteils Download PDF

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Publication number
EP3381602B1
EP3381602B1 EP18162546.8A EP18162546A EP3381602B1 EP 3381602 B1 EP3381602 B1 EP 3381602B1 EP 18162546 A EP18162546 A EP 18162546A EP 3381602 B1 EP3381602 B1 EP 3381602B1
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EP
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Prior art keywords
rené
cores
component
melting point
gtd
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English (en)
French (fr)
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EP3381602A1 (de
Inventor
Yan Cui
Srikanth Chandrudu Kottilingam
Brian Lee Tollison
Timothy Neal Pletcher
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GE Vernova GmbH
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General Electric Technology GmbH
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12—Both compacting and sintering
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/10—Metallic powder containing lubricating or binding agents; Metallic powder containing organic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12—Both compacting and sintering
    • B22F3/16—Both compacting and sintering in successive or repeated steps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/008—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression characterised by the composition
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00—Making metallic powder or suspensions thereof
    • B22F9/02—Making metallic powder or suspensions thereof using physical processes
    • B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00—Soldering, e.g. brazing, or unsoldering
    • B23K1/0008—Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K31/00—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by any single one of main groups B23K1/00 - B23K28/00
    • B23K31/02—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by any single one of main groups B23K1/00 - B23K28/00 relating to soldering or welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering or brazing
    • B23K35/0244—Powders, particles or spheres; Preforms made therefrom
    • B23K35/025—Pastes, creams or slurries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0255—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in welding
    • B23K35/0261—Rods, electrodes or wires
    • B23K35/0272—Rods, electrodes or wires with more than one layer of coating or sheathing material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0255—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in welding
    • B23K35/0261—Rods, electrodes or wires
    • B23K35/0277—Rods, electrodes or wires of non-circular cross-section
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
    • B23K35/0255—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in welding
    • B23K35/0261—Rods, electrodes or wires
    • B23K35/0283—Rods, electrodes or wires multi-cored; multiple
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550°C
    • B23K35/3033—Ni as the principal constituent
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550°C
    • B23K35/3046—Co as the principal constituent
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/40—Making wire or rods for soldering or welding
    • B23K35/404—Coated rods; Coated electrodes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/007—Alloys based on nickel or cobalt with a light metal (alkali metal Li, Na, K, Rb, Cs; earth alkali metal Be, Mg, Ca, Sr, Ba, Al Ga, Ge, Ti) or B, Si, Zr, Hf, Sc, Y, lanthanides, actinides, as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/07—Alloys based on nickel or cobalt based on cobalt
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
    • B22F7/04—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal
    • B22F2007/042—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal characterised by the layer forming method
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
    • B22F7/04—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal
    • B22F2007/042—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal characterised by the layer forming method
    • B22F2007/047—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal characterised by the layer forming method non-pressurised baking of the paste or slurry containing metal powder
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/34—Coated articles ; Surface treated articles

Definitions

  • the present invention is generally directed to a hybrid component and a method for treating a component using the hybrid component. More specifically, the present invention is directed to a hybrid component with multiple cores and a method for treating a component using the hybrid component.
  • Hard-to-weld (HTW) alloys such as nickel-based superalloys and certain aluminum-titanium alloys, due to their gamma prime and various geometric constraints, are susceptible to gamma prime strain aging, liquation and hot cracking. These materials are also difficult to join when the gamma prime phase is present in volume fractions greater than about 30%, which may occur when aluminum or titanium content exceeds about 3%.
  • an "HTW alloy” is an alloy which exhibits liquation, hot and strain-age cracking, and which is therefore impractical to weld.
  • HTW alloys may be incorporated into components of gas turbine engines such as airfoils, blades (buckets), nozzles (vanes), shrouds, combustors, rotating turbine components, wheels, seals, 3d-manufactured components with HTW alloys and other hot gas path components. Incorporation of these HTW alloys may be desirable due to often superior operational properties, particularly for certain components subjected to the most extreme conditions and stresses.
  • a method of treating a component according to the invention is defined in claim 7.
  • Embodiments of the present invention in comparison to methods and articles not utilizing one or more features disclosed herein, enable closing large openings of components of gas turbine engines without shrinkage and melting at a lower coast.
  • GTD 111 refers to an alloy including a composition, by weight, of about 14% chromium, about 9.5% cobalt, about 3.8% tungsten, about 4.9% titanium, about 3% aluminum, about 0.1% iron, about 2.8% tantalum, about 1.6% molybdenum, about 0.1% carbon, and a balance of nickel.
  • GTD 444" refers to an alloy including a composition, by weight, of about 7.5% cobalt, about 0.2% iron, about 9.75% chromium, about 4.2% aluminum, about 3.5% titanium, about 4.8% tantalum, about 6% tungsten, about 1.5% molybdenum, about 0.5% niobium, about 0.2% silicon, about 0.15% hafnium, and a balance of nickel.
  • HTYNES 188 refers to an alloy including a composition, by weight, of about 22% chromium, about 22% nickel, about 0.1% carbon, about 3% iron, about 1.25% manganese, about 0.35% silicon, about 14% tungsten, about 0.03% lanthanum, and a balance of cobalt.
  • INCONEL 738 refers to an alloy including a composition, by weight, of about 0.17% carbon, about 16% chromium, about 8.5% cobalt, about 1.75% molybdenum, about 2.6% tungsten, about 3.4% titanium, about 3.4% aluminum, about 0.1% zirconium, about 2% niobium, and a balance of nickel.
  • MAR-M-247 refers to an alloy including a composition, by weight, of about 5.5% aluminum, about 0.15% carbon, about 8.25% chromium, about 10% cobalt, about 10% tungsten, about 0.7% molybdenum, about 0.5% iron, about 1% titanium, about 3% tantalum, about 1.5% hafnium, and a balance of nickel.
  • René 108 refers to an alloy including a composition, by weight, of about 8.4% chromium, about 9.5% cobalt, about 5.5% aluminum, about 0.7% titanium, about 9.5% tungsten, about 0.5% molybdenum, about 3% tantalum, about 1.5% hafnium, and a balance of nickel.
  • René 142 refers to an alloy including a composition, by weight, of about 6.8% chromium, about 12% cobalt, about 6.1% aluminum, about 4.9% tungsten, about 1.5% molybdenum, about 2.8% rhenium, about 6.4% tantalum, about 1.5% hafnium, and a balance of nickel.
  • René 195" refers to an alloy including a composition, by weight, of about 7.6% chromium, about 3.1% cobalt, about 7.8% aluminum, about 5.5% tantalum, about 0.1% molybdenum, about 3.9% tungsten, about 1.7% rhenium, about 0.15% hafnium, and a balance of nickel.
  • Raé N2 refers to an alloy including a composition, by weight, of about 7.5% cobalt, about 13% chromium, about 6.6% aluminum, about 5% tantalum, about 3.8% tungsten, about 1.6% rhenium, about 0.15% hafnium, and a balance of nickel.
  • René N4 refers to an alloy including a composition, by weight, of about 9.75% chromium, about 7.5% cobalt, about 4.2% aluminum, about 3.5% titanium, about 1.5% molybdenum, about 6.0% tungsten, about 4.8% tantalum, about 0.5% niobium, about 0.15% hafnium, and a balance of nickel.
  • Raé N5 refers to an alloy including a composition, by weight, of about 7.5% cobalt, about 7.0% chromium, about 6.5% tantalum, about 6.2% aluminum, about 5.0% tungsten, about 3.0% rhenium, about 1.5% molybdenum, about 0.15% hafnium, and a balance of nickel.
  • Raé N500 refers to an alloy including a composition, by weight, of about 7.5% cobalt, about 0.2% iron, about 6% chromium, about 6.25% aluminum, about 6.5% tantalum, about 6.25% tungsten, about 1.5% molybdenum, about 0.15% hafnium, and a balance of nickel.
  • BNi-2 refers to an alloy including a composition, by weight, of about 3% iron, about 3.1% boron, about 4.5% silicon, about 7% chromium, and a balance of nickel.
  • BNi-5" refers to an alloy including a composition, by weight, of about 10% silicon, about 19% chromium, and a balance of nickel.
  • BNi-9 refers to an alloy including a composition, by weight, of about 15% chromium, about 3% boron, and a balance of nickel.
  • DF-4B refers to an alloy including a composition, by weight, of about 14% chromium, about 10% cobalt, about 3.5% aluminum, about 2.5% tantalum, about 2.75% boron, about 0.05% yttrium, and a balance of nickel.
  • hybrid preform component 100 includes a plurality of elongated metallic cores 101 and coating paste 102.
  • the coating paste 102 envelops the plurality of elongated metallic cores 101.
  • the plurality of elongated metallic cores 101 consist of an alloy selected from the group consisting of GTD 111, GTD 444, HAYNES 188, INCONEL 738, MAR-M-247, René 108, René 142, René 195, René N2, René N4, René N5, René N500, and combinations thereof.
  • coating paste 102 consists of a first material having a first melting point, a second material having a second melting point, and a binder.
  • the first melting point is greater than the second melting point.
  • the first melting point is greater than the second melting point by at least 5% or at least 10% or at least 20% or at least 30% or at least 40% or at least 50%.
  • the first material is a high melt material and the second material is a low melt material.
  • suitable first materials consist of an alloy selected from the group consisting of GTD 111, GTD 444, HAYNES 188, INCONEL 738, MAR-M-247, René 108, René 142, René 195, and René N2, or a combination thereof.
  • suitable second materials consist of an alloy selected from the group of DF-4B, BNi-2, BNi-5 (AMS 4782), BNi-9, or a combination thereof.
  • coating paste 102 has a first material in an amount, by weight, from 35% to 95% preferably from about 45% to about 85%, or from about 55% to about 75%, including increments, intervals, and sub-range therein.
  • coating paste 102 has a second material in an amount, by weight, from 5% to 65%, preferably from about 15% to about 55%, or from about 25% to about 45%, including increments, intervals, and sub-range therein.
  • a hybrid perform component 100 has a cross sectional ratio of the plurality of elongated metallic cores to the coating paste from about 40% to about 90%, from about 50% to about 80%, from about 60% to about 70%, including increments, intervals, and sub-range therein.
  • hybrid preform component 100 has a compressed structure and near net shape.
  • compressed structure refers to a structure that has been exposed to sufficient mechanical force to form a resilient structure capable of being exposure to additional processing.
  • near net shape refers to being of a geometry and size requiring little or no machining or processing after additive manufacturing.
  • hybrid preform component 100 includes two aligned elongated metallic cores 101 having the same diameter and joined together.
  • hybrid preform component 100 includes two aligned elongated metallic cores 101 having the same diameter and not joined together.
  • hybrid preform component 100 includes three aligned elongated metallic cores 101 having the same diameter and joined together.
  • hybrid preform component 100 includes three aligned elongated metallic cores 101 having the same diameter and not joined together.
  • hybrid preform component 100 includes three aligned elongated metallic cores 101 having dissimilar diameters and joined together.
  • hybrid preform component 100 includes three aligned elongated metallic cores 101 having dissimilar diameters and not joined together.
  • hybrid preform component 100 includes three non-aligned elongated metallic cores 101 having the same diameter and joined together.
  • hybrid preform component 100 includes three non-aligned elongated metallic cores 101 having the same diameter and not joined together.
  • hybrid preform component 100 includes three non-aligned elongated metallic cores 101 having dissimilar diameters and not joined together.
  • hybrid preform component 100 includes three non-aligned elongated metallic cores 101 having dissimilar diameters and not joined together.
  • hybrid preform component 100 includes three non-aligned elongated metallic cores 101 having dissimilar diameters and not joined together.
  • a hybrid perform component 100 has a cross-sectional geometry selected from the group consisting of a circle, an ellipse, an oval, a triangle, a rounded triangle, a square, a rounded square, a rectangle, a rounded rectangle, a pentagon, a rounded pentagon, a hexagon, a rounded hexagon, and a combination thereof.
  • those hybrid preform components 100 shown in FIGs. 12-22 may have elongated metallic cores with a variety of configurations as shown in FIGs. 2-11 .
  • the present invention may include more than three elongated metallic cores with a variety of configurations.
  • a method 200 for treating a component includes the step of mixing a first material having a first melting point, a second material having a second melting point, and a binder to make coating paste, wherein the first melting point is higher than the second melting point (step 201).
  • the method 200 further includes the step of assembling a plurality of cores (step 202).
  • the method further includes the step of coating the plurality of cores using the coating paste to form a coated rod assembly (step 203).
  • the method further includes the step of compressing the coated rod assembly to envelop the coating paste to the plurality of cores and form a preform component having a near net shape (step 204).
  • the method further includes the step of sintering the preform component to form a pre-sintered preform (step 205).
  • the preform component has a cross-sectional geometry including a circle, an ellipse, an oval, a triangle, a rounded triangle, a square, a rounded square, a rectangle, a rounded rectangle, a pentagon, a rounded pentagon, a hexagon, a rounded hexagon, or a combination thereof.
  • the method further includes the step of machining the pre-sintered preform to the required length and geometry (step 206). In one embodiment, the method further includes the step of brazing the pre-sintered preform in order to treat the component (step 207). In one embodiment, the method further includes the step of joining the plurality of cores. In one embodiment, a joining 103 includes resistance welding, tungsten inert gas tack welding, brazing, or a combination thereof. In one embodiment, the step of compressing may comprise extruding the coated rod assembly.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Composite Materials (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Claims (13)

  1. Hybride Vorformlingkomponente (100), umfassend:
    eine Vielzahl länglicher Metallkerne (101);
    eine Beschichtungspaste (102), die die Vielzahl länglicher Metallkerne (101) umhüllt, wobei die Beschichtungspaste (102) aus einem ersten Material mit einem ersten Schmelzpunkt, einem zweiten Material mit einem zweiten Schmelzpunkt und einem Bindemittel besteht, wobei der erste Schmelzpunkt höher ist als der zweite Schmelzpunkt, und wobei die Beschichtungspaste (102) das erste Material in einer Menge von 35 Gew.-% bis 95 Gew.-% und das zweite Material in einer Menge von 5 Gew.-% bis 65 Gew.-% aufweist,
    wobei die Vielzahl länglicher Metallkerne aus einer Legierung besteht, die aus der Gruppe ausgewählt ist, die aus GTD 111, GTD 444, HAYNES 188, INCONEL 738, MAR-M-247, René 108, René 142, René 195, René N2, René N4, René N5, René N500 und Kombinationen davon besteht,
    wobei das erste Material aus einer Legierung besteht, die aus der Gruppe ausgewählt ist, die aus GTD 111, GTD 444, HAYNES 188, INCONEL 738, MAR-M-247, René 108, René 142, René 195 und René N2 oder einer Kombination davon besteht,
    wobei das zweite Material aus einer Legierung besteht, die aus der Gruppe ausgewählt ist, die aus DF-4B, BNi-2, BNi-5 (AMS 4782), BNi-9 oder einer Kombination davon besteht, und
    wobei die hybride Vorformlingkomponente (100) eine komprimierte Struktur und eine endnahförmige Gestalt aufweist.
  2. Hybride Vorformlingkomponente (100) nach Anspruch 1, die ein Querschnittsverhältnis der Vielzahl länglicher Metallkerne (101) zur Beschichtungspaste (102) von etwa 40 % bis etwa 90 % aufweist.
  3. Hybride Vorformlingkomponente (100) nach einem der Ansprüche 1 bis 2, wobei die Vielzahl länglicher Metallkerne (101) den gleichen Durchmesser aufweist.
  4. Hybride Vorformlingkomponente (100) nach einem der Ansprüche 1 bis 2, wobei die Vielzahl länglicher Metallkerne (101) unterschiedliche Durchmesser aufweist.
  5. Hybride Vorformlingkomponente (100) nach einem der Ansprüche 1 bis 4, wobei die Vielzahl länglicher Metallkerne (101) miteinander verbunden ist.
  6. Hybride Vorformlingkomponente (100) nach einem der Ansprüche 1 bis 4, wobei die Vielzahl länglicher Metallkerne (101) nicht miteinander verbunden ist.
  7. Verfahren (200) zum Bearbeiten einer Komponente (100), umfassend:
    Mischen eines ersten Materials mit einem ersten Schmelzpunkt, eines zweiten Materials mit einem zweiten Schmelzpunkt und eines Bindemittels, um eine Beschichtungspaste (102) herzustellen, wobei der erste Schmelzpunkt höher als der zweite Schmelzpunkt ist, und wobei die Beschichtungspaste (102) das erste Material in einer Menge von 35 Gew.-% bis 95 Gew.-% und das zweite Material in einer Menge von 5 Gew.-% bis 65 Gew.-% aufweist;
    Anordnen einer Vielzahl von Kernen (101);
    Beschichten der Vielzahl von Kernen (101) unter Verwendung der Beschichtungspaste (102), um eine beschichtete Stabanordnung zu bilden;
    Komprimieren der beschichteten Stabanordnung, um die Vielzahl von Kernen (101) mit der Beschichtungspaste (102) zu umhüllen und eine Vorformlingkomponente (100) mit endnahförmiger Gestalt zu bilden;
    Sintern der Vorformlingkomponente (100) zu einem vorgesinterten Vorformling,
    wobei die Vielzahl von Kernen aus einer Legierung besteht, die aus der Gruppe ausgewählt ist, die aus GTD 111, GTD 444, HAYNES 188, INCONEL 738, MAR-M-247, René 108, René 142, René 195, René N2, René N4, René N5, René N500 und Kombinationen davon besteht,
    wobei das erste Material aus einer Legierung besteht, die aus der Gruppe ausgewählt ist, die aus GTD 111, GTD 444, HAYNES 188, INCONEL 738, MAR-M-247, René 108, René 142, René 195 und René N2 oder einer Kombination davon besteht, und
    wobei das zweite Material aus einer Legierung besteht, die aus der Gruppe ausgewählt ist, die aus DF-4B, BNi-2, BNi-5 (AMS 4782), BNi-9 oder einer Kombination davon besteht,
    wobei das Verfahren ferner das Löten des vorgesinterten Vorformlings an die Komponente umfasst.
  8. Verfahren (200) nach Anspruch 7, ferner umfassend das maschinelle Bearbeiten des vorgesinterten Vorformlings auf die erforderliche Länge und Geometrie.
  9. Verfahren (200) nach einem der Ansprüche 7 bis 8, wobei die Vielzahl von Kernen (101) den gleichen Durchmesser aufweist.
  10. Verfahren (200) nach einem der Ansprüche 7 bis 8, wobei die Vielzahl von Kernen (101) unterschiedliche Durchmesser aufweist.
  11. Verfahren (200) nach einem der Ansprüche 7 bis 10, ferner umfassend das Verbinden der Vielzahl von Kernen (101).
  12. Verfahren (200) nach einem der Ansprüche 7 bis 10, wobei die Vielzahl von Kernen (101) miteinander verbunden wird.
  13. Verfahren (200) nach einem der Ansprüche 7 bis 10, wobei die Vielzahl von Kernen (101) nicht miteinander verbunden ist.
EP18162546.8A 2017-03-29 2018-03-19 Hybridbauteil mit mehreren kernen und verfahren zur behandlung eines bauteils Active EP3381602B1 (de)

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AT315612B (de) 1971-07-27 1974-06-10 Ludwig Wozak Dipl Ing Verfahren und Elektroden zum Lichtbogenschweißen mit abschmelzenden Elektroden
US3989863A (en) 1975-07-09 1976-11-02 The International Nickel Company, Inc. Slurry coating process
DE10346281B4 (de) 2003-09-30 2006-06-22 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Verfahren zur Herstellung von Bauteilen mit einer Nickel-Basislegierung sowie damit hergestellte Bauteile
US8087565B2 (en) * 2008-09-08 2012-01-03 General Electric Company Process of filling openings in a component
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US10675686B2 (en) 2020-06-09

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